Спутник технологический. ZACUBE-1. [Редактировать]

КА ZACUBE-1 (South Africa CubeSat-1), массой 1 кг, изготовлен студентами Кейптаунского технологического университета и предназначен для отработки перспективных технологий.

Дополнительная классификация

#Наименования
1Страна оператор(владелец) - Южная Африка
2Страна производитель - Южная Африка

Технические характеристики

#ХарактеристикаЗначение
1Масса, кг1

Информация об удачном запуске

#ХарактеристикаЗначение
1Космодром Пусковая база Ясный
2Дата пуска2013-11-21 at 07:10:00 UTC
3Полезная нагрузка 1xAprizesat 7
4Полезная нагрузка 1xSkySat 1
5Полезная нагрузка 1xSTSAT 3
6Полезная нагрузка 1xDubaiSat 2
7Полезная нагрузка 1xWNISAT-1
8Полезная нагрузка 1xBRITE-PL
9Полезная нагрузка 1xAprizesat 8
10Полезная нагрузка 1xUniSat-5
11Полезная нагрузка 1xDelfi-n3Xr
12Полезная нагрузка 1xDove-3
13Полезная нагрузка 1xDove-4
14Полезная нагрузка 1xTriton-1
15Полезная нагрузка 1xCINEMA 1
16Полезная нагрузка 1xCINEMA 2
17Полезная нагрузка 1xOPTOS
18Полезная нагрузка 1xCubeBug-2
19Полезная нагрузка 1xGOMX-1
20Полезная нагрузка 1xNEE-02
21Полезная нагрузка 1xFUNcube-1
22Полезная нагрузка 1xHiNCube
23Полезная нагрузка 1xZACUBE-1
24Полезная нагрузка 1xICube-1
25Полезная нагрузка 1xHumSat-D
26Полезная нагрузка 1xPUCP-SAT-1
27Полезная нагрузка 1xFirst-MOVE
28Полезная нагрузка 1xUWE-3
29Полезная нагрузка 1xVELOX-P-2
30Полезная нагрузка 1xBeakerSat-1
31Полезная нагрузка 1x$50SAT
32Полезная нагрузка 1xQubeScout-S1
33Полезная нагрузка 1xWren
34Полезная нагрузка 1xPocket-PUCP
35Ракета-носитель 1xДнепр

Найдено 29 документов по запросу «ZACUBE-1». [Перейти к поиску]


Дата загрузки: 2017-01-04
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0.07/5
TshepisoSAT (ZACUBE-­‐1),   one  year  after  launch Leon  ...  March  2016 Introduction TshepisoSAT (ZACUBE-­‐1)  Mission TshepisoSAT (ZACUBE-­‐1)  Spacecraft Launch  and  ground...  Workshop  -­‐ San  Luis  Obispo 3 TshepisoSAT (ZACUBE-­‐1)  Mission • Space   weather   mission – Initiate...  Workshop  -­‐ San  Luis  Obispo 4 TshepisoSAT (ZACUBE-­‐1)  Spacecraft 15  March  2016 2015...  Workshop  -­‐ San  Luis  Obispo 5 TshepisoSAT (ZACUBE-­‐1)  Spacecraft • • • • • • • One  unit  (1U)  CubeSat...  Workshop  -­‐ San  Luis  Obispo 6 TshepisoSAT (ZACUBE-­‐1)  Spacecraft • Built  systems VHF/UHF...  Workshop  -­‐ San  Luis  Obispo 7 TshepisoSAT (ZACUBE-­‐1)  Software • Flight  software– C,  Pumpkin  Salvo...  Workshop  -­‐ San  Luis  Obispo 8 TshepisoSAT (ZACUBE-­‐1)  Launch • Delft  (ISIS)  – Netherlands • Yasny... (ZACUBE-­‐1)  Telemetry • Examined  parameters  from  two-­‐line  element  data   – Compared  ZACUBE-­‐1,  FUNcube...  -­‐ San  Luis  Obispo 12 TshepisoSAT (ZACUBE-­‐1)  Telemetry • Shows  HF  transmitter  is...  -­‐ San  Luis  Obispo 13 TshepisoSAT (ZACUBE-­‐1)  Telemetry • HF  antenna  deployment  motor...  -­‐ San  Luis  Obispo 14 TshepisoSAT (ZACUBE-­‐1)  Telemetry • Shows  one  burn  event...  -­‐ San  Luis  Obispo 15 TshepisoSAT (ZACUBE-­‐1)  Telemetry • Monitoring  roll  rates  through...  -­‐ San  Luis  Obispo 16 TshepisoSAT (ZACUBE-­‐1)  Images 15  March  2016 2015...  -­‐ San  Luis  Obispo 17 TshepisoSAT (ZACUBE-­‐1)  Lessons • What  would  we  do...  ZACUBE-­‐1  transceiver  and  S-­‐Band  transmitter  to  be   used  for  upcoming  ZACUBE-­‐2  mission...  Obispo 19 Thank  you TshepisoSAT (ZACUBE-­‐1),  one  year  after  launch Leon...  -­‐ San  Luis  Obispo 20 TshepisoSAT (ZACUBE-­‐1)  Telemetry 15  March  2016 2015...  -­‐ San  Luis  Obispo 21 TshepisoSAT (ZACUBE-­‐1)  Telemetry • On-­‐board  temperatures 15...  -­‐ San  Luis  Obispo 22 TshepisoSAT (ZACUBE-­‐1)  Spacecraft 15  March  2016 2015...  -­‐ San  Luis  Obispo 23 TshepisoSAT (ZACUBE-­‐1)  Layout 15  March  2016 2015...



Дата загрузки: 2016-12-25
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0.14/5
A Technical Background of the ZACUBE-i Satellite Mission Series Francois Visser Agenda • Roadmap ▫ In situ monitoring ▫ Remote sensing ▫ Space weather • Enabling Infrastructure ▫ Ground station ▫ AIT ▫ Mission assurance • CubeSat missions ▫ ZACUBE-1 ▫ ZACUBE-2 • Enabling technologies ▫ ▫ ▫ ▫ Comms ADCS Propulsion Radiation testing and hardening techniques ZACUBE-i Roadmap ZACUBE-i Space Weather Experiments 6 F’SATI 13 Apr 2010 SANSA Space Science, Hermanus SANAE Base Antarctica 7 ZACUBE-i Space Weather Experiments HF Antenna at SANAE-4 Part of the SuperDARN radar network ZACUBE-i Space Weather Experiments HF Ground Station Antenna Array Constructed at SANSA, Hermanus Designed and developed internally Infrastructure: Ground station • Typical amateur satellite tracking installation • VHF / UHF Amateur bands • Next phase: 2.4 m dish for S-band, C-band dish Infrastructure: AIT • Flight model integration and testing facilities • Clean room • New Electrical Engineering building ▫ 1000 m2 satellite development and production facilities Infrastructure: Mission Assurance • Access to other facilities in the region ▫ Hot vacuum and bakeout – iThemba Labs ▫ Vibration testing – Tellumat ▫ EMC testing – Anechoic chamber, Houwteq • To be acquired ▫ Thermal chamber ▫ Thermal vacuum chamber • Hardware-in-the-loop testing ▫ To be established by newly appointed research chair as a national facility ZACUBE-1 mission objectives • Space weather mission ▫ Initiate HF ionospheric propagation studies of ZACUBE-i series ▫ SuperDARN characterisation • Skills development ▫ ▫ ▫ ▫ Postgraduate students Establish infrastructure Professional development Building legacy • Technology demonstrator ▫ Deployable HF antenna ▫ UHF/VHF transceiver • Camera ▫ Awareness • Research output ▫ Conferences, journals, patents Time line • ZACUBE-1 ▫ 2011/12 ▫ 30 000 man/hrs ZACUBE-1 layout ZACUBE-1 HF beacon ZACUBE-1 Images ZACUBE-1 Telemetry ZACUBE-2 • 3U CubeSat • S-Band Transmitter • ADCS System Developed by ESL at Stellenbosch University • L-Band Receiver • VHF/UHF Communication System • HF Beacon Payload • On-Board Computer (OBC) • 5 MP Camera Payload ZACUBE-2 • ADCS ▫ Unique control method using aerodynamic drag ▫ Deployable UHF / L-band antennas also serve as stabilising tail feathers ▫ Deployable side panels control roll angle ▫ Full redundant backup with magnetorquers and reaction wheels. ▫ CubeSense ADCS sensor module • Space weather sensors to be determined • Collaboration with other institutions/universities in SA, Europe and America • Government approved funding for development QB50 Participation ZA-AeroSat • QB50 mission ▫ 50 International CubeSats with science payloads to model the upper layers of the thermosphere ▫ Launch January 2016 • ZA-AeroSat (Africa’s only contribution to QB50) ▫ SU project to design and manufacture 2U CubeSat ▫ F’SATI supplies comms payload – TT&C transceiver (CMC) and deployable antenna system ▫ Demonstrate passive aerodynamic stabilisation (antennae used like plumes on a shuttlecock) ▫ Fipex science sensor and new CubeStar star tracker CubeStar Enabling Technology: Communications • • • • S-band shorted annular ring patch antenna 7 dBi gain Circularly polarised Light weight: 17.2 g without screws • 89 x 83 x 4.3 mm Enabling Technology: Communications • S-band transmitter for large amounts of payload data ▫ 2 Mbps / 1 W RF transmit power ▫ QPSK modulation ▫ FEC ▫ Future improvements – 50 Mbps downlink – SDR – Transceiver: 10 Mbps uplink • UHF / VHF transceiver for telecommand / telemetry ▫ 1.2 kbps AFSK or 9.6 kbps GMSK amateur radio transceiver Enabling Technology • Nanosatellite propulsion, debris mitigation ▫ Wits University • ADCS ▫ ESL, Stellenbosch University • Radiation testing and hardening ▫ iThemba Labs ▫ University of Pretoria • Advanced manufacturing and nano-tech ▫ NLC, ALC Future nano-sat missions • Nano-satellite constellations provides a paradigm shift from existing platforms: ▫ High temporal resolution / medium ground sampling resolution – 30 min / 20 m vs. 8 hours / 10 m ▫ Shift in applications ▫ Technology threshold low ▫ Can be done by Africa, for Africa, in collaboration with our international partners The End



Дата загрузки: 2017-02-22
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0.26/5
...) beacon signal from the 1 U CubeSat ZACUBE 1 by the SuperDARN HF radar... of the HF beacon on ZACUBE 1 is to provide a continuous radio... 1 1 1.2 ZACUBE 1 CubeSat specifications . . . . . . . . . . . . . . . . . . . . . . . 1.3 Proposed instruments for tracking and receiving the ZACUBE 1 signal... List of Tables 3 (2009). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7 n 1.1 Proposed ZACUBE 1 orbital parameters and satellite characteristics... scientific payload for the 1 U CubeSat, ZACUBE 1. The CubeSat was developed by... actually reach the receiver, the ZACUBE 1 CubeSat specifications ity 1.2 of C actual... of ray tracing. ve rs ZACUBE 1v is a 1 U CubeSat with dimensions... was developed as a forerunner of ZACUBE 2, a 3 U prototype with dimensions 30 × 30... by Visser (2009). Table 1.1: Proposed ZACUBE 1 orbital parameters and satellite characteristics... area e The main payload of ZACUBE 1 is designed to emit an... IV in Antarctica of 1.3.1 C the ZACUBE 1 signal e Proposed instruments for tracking... to decode the signals from ZACUBE 1 and to verify the refraction... elevation angles. The visibility of ZACUBE 1, at an inclination angle of..., Prague, Czech Republic, 2010. Visser D., ZACUBE 1, 1U CubeSat: Mission Requirements and...



Дата загрузки: 2017-04-24
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0.07/5
... guessed ZACUBE-1, South Africa's first nanosatellite, then you are right. ZACUBE-1 was... of the payloads on-board ZACUBE-1 is a High Frequency (HF) radio... Figure 20: The components of ZACUBE-1 44 space weather research. It... the HF Beacon on-board ZACUBE-1 Figure 25: South African Air...



Дата загрузки: 2017-04-24
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0.15/5
... well. There was a document on ZACUBE-1, the first CubeSat by this...  A flight model 1-unit CubeSat called ZACUBE-01 was developed and prepared....  Another 3-unit CubeSat prototype called ZACUBE-02 is being built  For..., CPUT/EMSS Antennas (part-time) ZACUBE-01 Development Team Mr Charl... Research and Innovation (R&I) Centre registration  ZACUBE mission definition  List of Alumni...



Дата загрузки: 2017-03-18
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0.2/5
F’SATI Postgraduate Programme in Satellite Systems Engineering The First African CubeSat, ZACUBE-01 7 August 2011 Renier Siebrits siebritsr@cput.ac.za 1 Overview • The F’SATI satellite programme • 1U CubeSat Mission – Mission – Objectives – Subsystems – Design Challenges • Other Projects 7 August 2011 F’SATI 2 F’SATI Space Phase 1: Academic coursework Phase 3: Engineers in Training Programme (flight model) 2009 1U launch Phase 2: Research project (prototype design) 2010 2011 F’SATI 2012 2013 3 Engineers In Training Program • 8 Engineers in Training • Main Objective – Design and build a 1U CubeSat in 1 Year 7 August 2011 F’SATI 4 Define a Mission • SANSA: Space Science – South African National Space Agency • Space Weather Monitoring • Ionospheric Studies 7 August 2011 F’SATI 5 SuperDARN Radar System • Super Dual Auroral Radar Network • Ionospheric Studies • Radars in Northern and Southern Hemisphere • HF Frequency Bands ( 8 to 22 MHz) • Calibration of SANAE Base Radar System 7 August 2011 F’SATI 6 SANSA: Space Science Cape Town SANAE Base Antarctica 13 Apr 2010 F’SATI 7 SANAE Base Antarctica 13 Apr 2010 F’SATI 8 SuperDARN Radar Antennas 13 Apr 2010 F’SATI 9 13 Apr 2010 F’SATI 10 Mission Challenges • Orbit Inclination 98° 13 Apr 2010 65° F’SATI 11 Mission Challenges • HF Frequency Range 7 August 2011 F’SATI 12 IONOSPHERE 13 Apr 2010 F’SATI 13 Lowest Frequency: 8 MHz IONOSPHERE 13 Apr 2010 F’SATI 14 Mission Challenges • HF Frequency Range – Received Licensing for 14.099 MHz • Antenna – 14.099 MHz – Full Wavelength: 21.28 m or 69.81 ft – Monopole Length: 5.32 m or 17.45 ft 7 August 2011 F’SATI 15 ZACUBE-01 Specifications • Bought in Items: – 1U Structure – Clyde Space EPS, Battery & Solar Panels – ISIS VHF/UHF Antenna – Pumpkin OBC 7 August 2011 F’SATI 16 ZACUBE-01 Specifications • In-House Developed Subsystems: – VHF/UHF Transceiver • 145.86 MHz Uplink • 437.345 MHz Downlink – Payload Board • HF Beacon Transmitter • ADCS • Camera Payload – HF Antenna Deployment Mechanism 7 August 2011 F’SATI 17 • VHF/UHF Antenna • Antenna Deployment Mechanism • ADCS/camera/HF Beacon • EPS & Battery • VHF/UHF Transceiver • OBC • Deployable Magnetometer 13 Apr 2010 F’SATI 18 13 Apr 2010 F’SATI 19 13 Apr 2010 F’SATI 20 13 Apr 2010 F’SATI 21 Subsystem Progress • Completed: – Camera, HF Beacon, ADCS • Work in Progress: – Mechanical Manufacturing – VHF/UHF Transceiver – Flight Software • Launching 2012 7 August 2011 F’SATI 22 Other Projects: CanSats 13 Apr 2010 F’SATI 23 13 Apr 2010 F’SATI 24 Other Projects - STX • 2.4 – 2.48 GHz • 1 Watt RF Power • 2 Mbps Data Rate • 6 W Power Consumption • QPSK Modulation 13 Apr 2010 F’SATI 25 Ground Station 13 Apr 2010 F’SATI 26 IAC and CubeSat Workshop • International Astronautical Congress – Cape Town International Convention Centre – 3 - 7 October 2011 • 1st International African Cubesat Workshop – 30 September to 2 October 7 August 2011 F’SATI 27 Thank You! Contact Personal: • Prof Robert van Zyl • vanzylr@cput.ac.za • Francois Visser • visserdf@cput.ac.za • Renier Siebrits • siebritsr@cput.ac.za 13 Apr 2010 www.cput.ac.za/fsati F’SATI 28



Дата загрузки: 2016-11-03
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0.04/5
... announced that a nanosatellite known as ZACUBE-1, weighing 1.2 kg, would be launched...’s and Africa’s first nanosatellite.54 ZACUBE-1 payload is to include a High... technology.”56 The launch of ZACUBE-1 has been delayed until mid..., “ZACUBE-1,” 2013, online: https://directory.eoportal.org/web/eoportal/ satellite-missions/v-w-x-y-z/zacube...



Дата загрузки: 2017-01-30
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0.08/5
... студентами норвежских университетов. 27 КА ZACUBE-1 (South Africa CubeSat-1) изготовлен студентами..., Великобритания, 1 кг GOMX 1, Дания, 2 кг ZACUBE 1, Южная Африка, 1 кг NEE 02...



Дата загрузки: 2017-02-06
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0.11/5
...-P2 skCube Dynacube ZA-AeroSat ZACUBE-1 ZACUBE-2 CINEMA-2 (KHUSAT 1) CINEMA-3 (KHUSAT 2) Deployable...



Дата загрузки: 2017-02-06
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0.12/5
... Krysaor HiNCube (Høgskolen i Narvik CubeSat) ZACUBE 1 ((South Africa CubeSat-1) or TshepisoSat... Palydovas funkcionuoja Pietų Afrika 175 1 ZACUBE 1 Žemės jonosferos tyrimas; Pietų pa...